Locking actuator stem and rod end bearing apparatus for use with fluid valves

Actuator stem and rod end bearings having locking mechanisms are described. An example apparatus for use with a control valve actuator includes a rod end bearing having a bearing retainer and a shaft portion extending from the bearing retainer. The apparatus also includes an actuator stem having a first end to be operatively coupled to a diaphragm plate of the control valve actuator and a second end to be coupled to the rod end bearing. A locking mechanism coupled to the actuator stem or the rod end bearing prevents the actuator stem and the rod end bearing from decoupling when the actuator stem is coupled or de-coupled to the diaphragm plate.

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Description
FIELD OF THE DISCLOSURE

This disclosure relates generally to valve actuators and, more particularly, to locking actuator stem and rod end bearing apparatus for use with fluid valves.

BACKGROUND

Automated control valves such as, for example, rotary control valves, are often used in process control plants or systems to control the flow of process fluids. A rotary control valve typically includes an actuator (e.g., a pneumatic actuator, an electric actuator, a hydraulic actuator, etc.) operatively coupled to a shaft extending from the rotary valve via a lever. The lever converts a rectilinear displacement of an actuator stem into a rotational displacement of the valve shaft. Thus, rotation of the lever causes the valve shaft and a flow control member (e.g., a disk, a ball, etc.) coupled to the valve shaft to rotate to increase or restrict fluid flow through the valve.

To couple the lever to the actuator stem, a rod end bearing is typically employed. The rod end bearing may include an internally threaded bore (i.e., a female connection) that threadably receives an externally threaded end (i.e., a male connection) of the actuator stem. Alternatively, the rod end bearing may include an externally threaded end that threadably couples to an internally threaded bore of the actuator stem.

In some cases, a chemical thread locking gel may be employed to lock the threads of the actuator stem and rod end bearing connection. However, such locking gels may not provide sufficient locking strength and may allow the rod end bearing and the actuator stem to decouple even when a small amount of torque is applied during disassembly of the actuator (e.g., removal of a diaphragm cap screw).

SUMMARY

In one example, an example apparatus for use with a control valve actuator includes a rod end bearing having a bearing retainer and a shaft portion extending from the bearing retainer. The assembly also includes an actuator stem having a first end to be operatively coupled to a diaphragm plate of the control valve actuator and a second end to be coupled to the rod end bearing. A locking mechanism coupled to the actuator stem or the rod end bearing prevents the actuator stem and the rod end bearing from decoupling when the actuator stem is coupled or decoupled to the diaphragm plate.

In another example, an example apparatus for use with control valve actuators includes means for coupling a rod end bearing and an actuator stem to provide a rod end bearing and actuator stem connection for use with rotary valve actuators. The assembly also includes means for locking the rod end bearing and the actuator stem when coupled together via the means for coupling, where the means for locking is integrally formed with the rod end bearing or the actuator stem and prevents the actuator stem from decoupling from the rod end bearing.

In yet another example, an example apparatus for use with a valve actuator includes a rod end bearing and an actuator stem. A threaded member threadably couples the rod end bearing and the actuator stem. At least one of the rod end bearing, the actuator stem, or the threaded member includes a deformable portion to prevent inadvertent separation of the rod end bearing and actuator stem or to permit relative rotation of the rod end bearing and the actuator stem in one direction only.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 illustrates a known example rotary valve actuator having an externally threaded rod end bearing coupled to an internally threaded bore of an actuator stem.

FIG. 2 illustrates an example rotary valve actuator implemented with an example rod end bearing and actuator stem connection described herein.

FIG. 3A illustrates an enlarged partial view of the example rod end bearing and actuator stem connection of FIG. 2.

FIG. 3B illustrates a cross-sectional view of the example rod end bearing and actuator stem connection illustrated in FIG. 3A.

FIGS. 4A-4D illustrate yet another example rod end bearing and actuator stem connection described herein.

FIG. 5 illustrates yet another example rod end bearing and actuator stem connection described herein.

FIGS. 6A-6C illustrate yet another example rod end bearing and actuator stem connection described herein.

FIGS. 7A-7D illustrate yet another example rod end bearing and actuator stem connection described herein.

FIG. 8 illustrates yet another example rod end bearing and actuator stem connection described herein.

FIGS. 9A-9C illustrate yet another example rod end bearing and actuator stem connection described herein.

 DETAILED DESCRIPTION

In general, the example apparatus described herein prevent inadvertent decoupling of a connection between a rod end bearing and an actuator rod or stem of a control valve actuator. In particular, the example apparatus include a rod end bearing and an actuator stem having an (e.g., integrally formed) anti-rotation or locking mechanism to prevent disassembly of the rod end bearing and the actuator stem during, for example, maintenance or repair of an actuator. For example, a rod end bearing and actuator stem connection described herein can prevent decoupling of the connection even if a relatively large amount of torque applied to a fastener when coupling and/or removing a diaphragm plate to and/or from the end of the actuator stem opposite the end coupled to the rod end bearing. In contrast to many known devices, the anti-rotation or locking mechanisms described herein do not require chemicals (e.g., thread locking compounds), additional parts, or components.

FIG. 1 is a cross-sectional view of a known control valve actuator or actuator assembly 100 that may be used with, for example, a rotary fluid valve. Referring in detail to FIG. 1, the example actuator assembly 100 includes an actuator 102 coupled to a housing 104. The actuator 102 includes a casing 106 that captures a diaphragm 108 between an upper casing portion 110 and a lower casing portion 112. The casing portions 110 and 112 are coupled together with a plurality of threaded fasteners 114 spaced along an outer edge of the casing 106. The diaphragm 108 separates the space within the casing 106 into a control pressure chamber 116 through which a controlled pressure is supplied via an inlet port 118 to displace the diaphragm 108. A diaphragm plate 120 couples the diaphragm 108 to an actuator stem or diaphragm rod 122 and provides a rigid backing for the diaphragm 108. The actuator stem 122 includes a first end 124 having an internally threaded bore 126 that receives a fastener 128 (e.g., a cap screw) to couple the diaphragm plate 120 to the actuator stem 122.

Springs 130, 132, and 134 surround the actuator stem 122 and are disposed between the diaphragm plate 120 and respective spring seats 136, 138, and 140 integrally formed as shoulders on the lower casing 112. Each of the springs 130, 132, and 134 provides a biasing force against the diaphragm plate 120 to return the actuator stem 122 and any suitable operator (e.g., a flow control member of a rotary valve) coupled to the actuator stem 122 to a known position in the absence of a control pressure applied to the diaphragm 108. The actuator stem 122 rotatably couples to a lever 142 via a rod end bearing 144.

The rod end bearing 144 includes a bearing retainer or body 146 having a stem, shaft or shank 148 extending therefrom. The retainer body 146 rotatably couples to the lever 142 and the shaft 148 couples to the actuator stem 122. At least a portion of the shaft 148 includes external threads 150 that threadably couple to an internally threaded bore 152 at a second end 154 of the actuator stem 122. However, in other examples, the shaft 148 of the rod end bearing 144 may include an internally threaded bore that receives an externally threaded portion of the actuator stem 122.

During assembly of the actuator assembly 100, the rod end bearing 144 is coupled to the actuator stem 122 and disposed within the housing 104. The springs 130, 132, and 134 are then disposed in the actuator casing 106 to surround the actuator stem 122. The diaphragm plate 120 is then coupled to the actuator stem 122 via the fastener 128. As the fastener 128 is tightened, the diaphragm plate 120 compresses the springs 130, 132, and 134, which provides a preload condition. The torque applied to tighten the fastener 128 causes the actuator stem 122 to angularly deflect, thereby transmitting a torsional load to the rod end bearing and actuator stem connection 156.

In some instances, during disassembly of the actuator assembly 100 for maintenance, replacement of components, and/or any other purpose, when the fastener 128 is loosened, the actuator stem 122 may rotate relative to the rod end bearing 144 and may cause the actuator stem 122 to loosen relative to and/or decouple from the rod end bearing 144. As a result, the springs 130, 132 and 134 may exit from the casing 106.

To prevent the actuator stem 122 and/or the rod end bearing 144 from loosening or decoupling when the cap screw 128 is loosened, a chemical thread locking gel (not shown) is often used to lock the threads of the actuator stem 122 and rod end bearing 144. However, such chemical locking gels increase manufacturing costs and may not provide adequate strength to prevent the actuator stem 122 and rod end bearing 144 from decoupling (i.e., unthreading) during, for example, disassembly of the diaphragm plate 120 and the actuator stem 122. For example, even with the use of such a chemical locking gel, disassembly or decoupling of the actuator stem and rod end bearing connection 156 may occur when a relatively low torque is applied to the cap screw 128. Although the actuator assembly 100 of FIG. 1 illustrates a pneumatic actuator 102, the example actuator assembly 100 may be implemented with other types of actuators such as, for example, an electric actuator, a hydraulic actuator, etc.

FIG. 2 illustrates an example control valve actuator or actuator assembly 200 implemented with an example rod end bearing and actuator stem connection 202 described herein. Those components of the example actuator assembly 200 of FIG. 2 that are substantially similar or identical to those components of the example actuator assembly 100 described above and that have functions substantially similar or identical to the functions of those components will not be described in detail again below. Instead, the interested reader is referred to the above corresponding descriptions in connection with FIG. 1. Those components that are substantially similar or identical will be referenced with the same reference numbers as those components described in connection with FIG. 1.

In the illustrated example of FIG. 2, an actuator stem 204 includes a first end 206 having an internally threaded bore 208 that may be any suitable length (e.g., to prevent the threads from stripping due to tightening). A rod end bearing or spherically shaped bearing 210 includes a bearing retainer or body 212 having a stem, shaft or shank 214 extending therefrom. The shaft 214 includes an internally threaded bore 216 that may be any suitable length. An externally threaded stud 218 threadably engages the bores 208 and 216 to couple the actuator stem 204 and the rod end bearing 210. The actuator stem 204 also includes a second end 220 having an internally threaded bore 222 that receives the fastener 128 to couple the actuator stem 204 to the diaphragm plate 120 and the diaphragm 108. As the diaphragm plate 120 is fastened to the actuator stem 204, the springs 130, 132, and 134 compress to provide a preload. Additionally, during assembly of the actuator assembly 200, the torque applied to the fastener 128 to couple the diaphragm plate 120 to the actuator stem 204 transmits a torsional load to the actuator stem 204, causing the actuator stem 204 to angularly deflect and/or rotate. When assembled, the actuator stem 204 and the rod-end bearing 210 retain the springs 130, 132, and 134 under compression within the housing 112 of the actuator assembly 200.

As described in greater detail below in connection with FIGS. 3A and 3B, the connection 202 provides an anti-rotation or locking mechanism configured to prevent rotation of the actuator stem 204 relative to the rod end bearing 210 once the actuator stem 204 is coupled to the rod end bearing 210. For example, when disassembling the actuator assembly 200 during, for example, maintenance, the cap screw 128 is loosened. The connection 202 prevents the actuator stem and the rod end bearing connection 202 from becoming loose, even when a relatively high torque is applied to the fastener 128 as the fastener 128 is loosened (e.g., turned in a counterclockwise direction). Thus, the connection 202 prevents the actuator stem 204 and the rod end bearing 210 from decoupling, unthreading or separating when the fastener 128 is removed from the diaphragm plate 120 and the actuator stem 204. The connection 202 is configured to enable assembly of the actuator stem 204 and the rod end bearing 210 using a relatively low torque, while preventing disassembly or requiring a relatively high torque to disassemble or decouple the actuator stem 204 from the rod end bearing 210.

FIG. 3A illustrates the example actuator stem 204 and rod end bearing 210 of FIG. 2. FIG. 3B illustrates a partial cross-sectional enlarged view of the example actuator stem 204 and the rod end bearing 210 of FIG. 3A.

Referring to FIGS. 3A and 3B, the rod end bearing 210 is coupled to the first end 206 of the actuator stem 204 via the externally threaded stud 218. In this example, the actuator stem 204 and the shaft 214 of the rod end bearing 210 have cylindrically-shaped bodies. The actuator stem 204 includes an opening 302 having an axis 304 that is substantially perpendicular to an axis 306 of the actuator stem 204. The opening 302 extends from an outer surface 308 of the actuator stem 204 to an inner surface 310 of the bore 208. As shown in this example, the rod end bearing 210 also includes an opening 312 having an axis 314 substantially perpendicular to the axis 306. The opening 312 extends from an outer surface 316 of the rod end bearing 210 to an inner surface 318 of the bore 216. In other examples, the actuator stem 204 and/or the rod end bearing 210 may include a plurality of openings along the respective ends 206 and 214 of the actuator stem 204 and/or the rod end bearing 210. In yet other examples, the openings 302 and/or 312 may be a slot, an elongated slot, an angled opening, an angled slot or any other opening.

A relatively low torque is required to couple the actuator stem 204 to the rod end bearing 210 when the actuator stem 204 and the rod end bearing 210 are assembled via the threaded stud 218. In the illustrated example, once assembled, at least a portion of the threads 320a of the stud 218 are exposed via the opening 302 and another portion of the threads 320b of the stud 218 are exposed via the opening 312. In this manner, the exposed threads 320a and/or 320b of the stud 218 may be deformed (e.g., plastically deformed) via, for example, a punch or any other suitable tool (e.g., inserted via the respective openings 302 and 312). Such deformation of the threads 320a and/or 320b provides an anti-rotation or locking mechanism to prevent inadvertent disassembly of the actuator stem 204 and the rod end bearing 210. In other words, a substantial amount of torque would be required to turn the actuator stem 204 relative to the rod end bearing 210 to decouple or disengage the actuator stem 204 and the rod end bearing 210 when the exposed threads 320a and/or 320b are deformed.

Thus, the locking mechanism of FIGS. 2, 3A and 3B provides a locked condition between rod end bearing 210 and the actuator stem 204 to further resist torsional load and angular deflection that may be experienced by the actuator stem 204 when the fastener 128 is loosened or turned (e.g., in a counter-clockwise direction) about the axis 306.

FIG. 4A illustrates yet another example actuator stem and rod end bearing connection 400 described herein that may be used to implement, for example, the actuator assembly 100 of FIG. 1. FIGS. 4B and 4C illustrate end views of an example actuator stem 402 and a rod end bearing 404 of FIG. 4A. FIG. 4D illustrates a cross-sectional side view of the example actuator stem and the rod end bearing connection 400 taken along line 4D-4D of FIG. 4A.

Referring to FIGS. 4A-4D, the actuator stem 402 and the rod end bearing 404 include respective threaded bores 406 and 408 at respective first ends 410 and 412 of the actuator stem 402 and the rod end bearing 404. The bores 406 and 408 are sized to receive an externally threaded stud 414 to couple the actuator stem 402 and the rod end bearing 404.

Referring to FIGS. 4B and 4C, in this example, the first end 410 of the actuator stem 402 includes a face or surface 416 (FIG. 4B) having a shape or geometry to matably engage or interlock with a complementary shape or geometry of a face or surface 418 (FIG. 4C) of the rod end bearing 404. The faces 416 and 418 of the respective actuator stem 402 and rod end bearing 404 interlock to provide an anti-rotation or locking mechanism when the actuator stem 402 is coupled to the rod end bearing 404. More specifically, in this example, and as most clearly shown in FIGS. 4B and 4C, the face 416 of the actuator stem 402 and the face 418 of the rod end bearing 404 have a plurality of serrations 420 such as, for example, sawtooth-shaped portions 422 and 424. For example, the sawtooth-shaped portions 422 of the actuator stem 402 are adapted to matably engage the corresponding or complementary sawtooth-shaped portions 424 of the rod end bearing 404.

Referring to FIG. 4D, coupling the actuator stem 402 and the rod end bearing 404 causes the teeth or sawtooth-shaped portions 422 to engage with the teeth or the sawtooth-shaped portions 424 to provide an anti-rotation or locking mechanism. In particular, referring to FIG. 4D, each of the sawtooth-shaped portions 422 and 424 includes a sloped surface or edge 426 and a locking surface 428. The sloped edges 426 of the sawtooth-shaped portions 422 and 424 enable the actuator stem 402 to rotate in a first direction (e.g., a clockwise direction) relative to the rod end bearing 404 about an axis 430. However, the locking surface 428 of each of the sawtooth-shaped portions 422 and 424 engage to prevent rotation of the actuator stem 402 in a second direction (e.g., a counterclockwise direction) relative to the rod end bearing 404 about the axis 430.

When the example actuator stem 402 and rod end bearing 404 are coupled to, for example, the actuator assembly 100 of FIG. 1, the sloped edges 426 enable the actuator stem 402 to rotate (e.g., in a clockwise direction) relative to the rod end bearing 404 when the fastener 128 is rotated (e.g., a torque is applied to the fastener 128 in a clockwise direction) about the axis 430 during assembly of the diaphragm plate 120 and the actuator stem 402. However, during disassembly, the locking surfaces 428 engage to prevent rotation of the actuator stem 402 relative to the rod end bearing 404 when the fastener 128 is rotated (e.g., when a torque is applied to the fastener 128 in a counterclockwise direction) about the axis 430 to disassemble the diaphragm plate 120 from the actuator stem 402. Alternatively, in other examples, only a portion of the face 416 and/or the face 418 may include serrations 420, sawtooth-shaped portions 422 and 424 and/or any other suitably shaped portions.

The example anti-rotation or locking mechanisms are not limited to the serrations 420 or sawtooth-shaped portions 422 and 424 illustrated in FIGS. 4A-4D. FIG. 5 illustrates another example actuator stem and rod end bearing connection 500 described herein that provides an anti-rotation or locking mechanism. In the illustrated example, only a portion of a face 502 of an actuator stem 504 and a portion of a face 506 of a rod end bearing 508 include serrations or other suitable complementary-shaped portions. In the illustrated example, the face 502 of the actuator stem 504 includes protruding members 510 and the face 506 of the rod end bearing 508 includes complementary recessed or grooved portions 512. The recessed portions 512 are sized and/or shaped to receive or matably engage with the protruding members 510 when the actuator stem 504 and the rod end bearing 508 are coupled together. When assembled, the protruding members 510 engage the recessed portion 512 to prevent rotation of the actuator stem 504 relative to the rod end bearing 508 when, for example, the actuator stem 504 and the rod end bearing 508 are coupled to the example actuator assembly 100 of FIG. 1 and the fastener is rotated (e.g., in a counterclockwise direction) relative to the actuator stem 504.

FIGS. 6A-6C illustrate yet another example actuator stem and rod end bearing connection 600 described herein providing an anti-rotation or locking mechanism. In this example, an actuator stem 602 and a rod end bearing 604 include respective apertures 606 and 608 to receive a pin or stud 610 (e.g., a non-threaded stud, an externally threaded stud, etc.). A first face or end 612 of the actuator stem 602 and a first face or end 614 of the rod end bearing 604 include helically-shaped ends. The ends 612 and 614 include respective sloped or curved surfaces 616a and 616b forming respective wedges, shoulders or locking surfaces 618a and 618b. When coupled together, the sloped surfaces 616a and 616b enable rotation of the actuator stem 602 relative to the rod end bearing 604 in a first direction about an axis 620. However, the shoulders or locking surfaces 618a and 618b prevent rotation of the actuator stem 602 relative to the rod end bearing 604 in a second direction opposite the first direction about the axis 620.

When the example actuator stem 602 and rod end bearing 604 are coupled to, for example, the actuator assembly 100 of FIG. 1, the ends 612 and 614 matably engage to provide an anti-rotation or locking mechanism. During assembly of the diaphragm plate 120 and the actuator stem 602, the sloped surfaces 616 enable the actuator stem 602 to rotate (e.g., in a clockwise direction) relative to the rod end bearing 604 about the axis 620 when the fastener 128 is tightened or rotated (e.g., when a torque is applied to the fastener 128 in a clockwise direction). However, during disassembly of the diaphragm plate 120 and the actuator stem 602, the shoulders or locking surfaces 618a and 618b engage to prevent rotation of the actuator stem 602 relative to the rod end bearing 604 about the axis 620 when the fastener 128 is loosened or rotated (e.g., when a torque is applied to the fastener 128 in a counterclockwise direction) about the axis 620.

FIG. 7A is a partial cross sectional view of yet another example actuator stem and rod end bearing connection 700 providing an anti-rotation or locking mechanism. FIG. 7B illustrates an example stud or pin 704. FIG. 7C illustrates a partial view of an example actuator stem 702 of FIG. 7A. FIG. 7D is a cross-sectional view of the actuator stem 702 of FIG. 7C taken along line 7D-7D.

Referring to FIGS. 7A and 7B, the actuator stem 702 is coupled to a rod end bearing 706 via the stud 704. In the illustrated example, the stud 704 includes first and second threaded ends or portions 708 and 710 and a recessed portion or reduced shank 712 between the threaded portions 708 and 710. The diameter of each of the threaded portions 708 and 710 is larger than the diameter of the recessed portion 712. In this manner, the recessed portion 712 forms a first shoulder 714 adjacent the first threaded portion 708 and a second shoulder 716 adjacent the second threaded portion 710. The actuator stem 702 and the rod end bearing 706 include threaded bores 718 and 720 to receive the respective first and second threaded portions 708 and 710 of the stud 704. In other examples, the first and second ends 708 and 710 are non-threaded and are received by respective non-threaded bores of the actuator stem 702 and the rod end bearing 706.

Referring also to FIGS. 7C and 7D, in the illustrated example, the actuator stem 702 and the rod end bearing 706 include respective tabs or deflectable members 722a and 722b. The tab 722a is disposed along (e.g., integrally formed with) a body 724 of the actuator stem 704 and the tab 722b is disposed along (e.g., integrally formed with) a body 726 of the rod end bearing 706. The tabs 722a and 722b may be formed via a punching operation or any other suitable manufacturing process. When the actuator stem 702 is coupled to the rod end bearing 706, the tabs 722a and 722b are pressed or deformed (e.g., plastically deformed) toward the stud 704 via, for example, a tool.

When the tabs 722a and 722b are deformed toward the stud 704, the tabs 722a and 722b engage the respective first and second shoulders 714 and 716 of the stud 704 to provide a locking mechanism or locked condition. In this manner, the tabs 722a and/or 722b prevent the actuator stem 702 from disengaging or decoupling from to the rod end bearing once the tabs 722a or 722b are deformed to engage the shoulders 714 and 716 of the stud 704. For example, FIG. 7C illustrates a perspective view of a portion of the actuator stem 702 showing the tab 722a in a depressed or deformed condition. FIG. 7D illustrates a cross-sectional view taken along line 7D-7D of FIG. 7C showing the tab 722a in a depressed or deformed condition relative to the body 724 of the actuator stem 702.

In operation, when coupled to, for example, the example actuator assembly 100 of FIG. 1, the tabs 722a and/or 722b provide a locking mechanism to prevent the actuator stem 702 from disengaging or decoupling from or rotating relative to the rod end bearing 706 when a torque is applied to the fastener 128 (e.g., in a counterclockwise direction) about an axis 728. In other examples, either or both of the actuator stem 702 or the rod end bearing 706 may include tabs or deformable members such as the tabs 722a or 722b. In yet other examples, the actuator stem 702 and/or the rod end bearing 706 may include a plurality of such tabs or deformable members.

FIG. 8 illustrates yet another example actuator stem and rod end bearing connection 800 providing a locking mechanism. In this example, a rod end bearing 802 includes a stem or shaft 804 protruding from a body or bearing 806 of the rod end bearing 802. The shaft 804 includes a head portion 808 having a first diameter that is larger than a diameter of the shaft 804 to form or provide a shoulder 810 adjacent the head portion 808. An actuator stem 812 includes a bore 814 that is sized to receive the head portion 808 of the shaft 804. In this example, the actuator stem 812 also includes tabs 816 that are integrally formed with a body 818 of the actuator stem 812 via, for example, machining.

When assembled, the bore 814 of the actuator stem 812 receives the head portion 808 of the shaft 804 of the rod end bearing 810. The head portion 808 is disposed within the bore 814 until the head portion 808 moves adjacent (e.g., moves past) the tabs 816 of the actuator stem 812. The tabs 816 are then deformed (e.g., plastically deformed) via, for example, a tool to engage the shoulder 810 formed by the head portion 808 and the shaft 804. In this manner, the tabs 816 provide a locking mechanism to lock the actuator stem 812 and the rod end bearing 802 together and prevent disassembly of the actuator stem 812 and the rod end bearing 802.

When coupled to, for example, the actuator assembly 100 of FIG. 1, the tabs 816 prevent the actuator stem 812 and the rod end bearing 802 from disengaging or decoupling when a torque is applied to the fastener 128 (e.g., in a counterclockwise direction) about an axis 820 during disassembly of the diaphragm plate 120 and the actuator stem 812. In other words, even if the actuator stem 812 rotates relative to the rod end bearing 802, the tabs 816 engage the shoulder 810 to provide a locking mechanism that prevents the actuator stem 812 from disengaging or decoupling from the rod end bearing 802.

FIGS. 9A-9C illustrate yet another example actuator stem and rod end bearing connection 900 having a locking mechanism. In this example, a rod end bearing 902 includes a stem or shaft 904 protruding from an end 906 of the rod end bearing 902. The shaft includes a head portion 908 and a threaded portion 910. The head portion 908 is sized larger than the shaft 904 (e.g., the head portion 908 has a diameter greater than a diameter of the shaft 904) to form a shoulder 912. The shaft 904 may be formed via for example, machining and/or any other suitable manufacturing process(es).

An actuator stem 914 has an internally threaded bore 916 that is sized to receive the threaded portion 910 of the rod end bearing 902. Additionally, an end 918 of the actuator stem 914 includes fingers or deflectable members 920 protruding from the actuator stem 914 that can deflect (e.g., elastically deform) relative to the actuator stem 914. Each of the fingers 920 includes a lip or protruding tab 922. The actuator stem 914 may be formed via, for example, machining and/or any other suitable manufacturing process(es).

During assembly, the threaded portion 910 of the shaft 904 of the rod end bearing 902 threadably engages the threaded bore 916 of the actuator stem 914. As the shaft 904 threads into the threaded bore 916, the head portion 908 engages the tabs 922 of the fingers 920 causing the fingers 920 to deflect (e.g., elastically deflect) outward or away from the actuator stem 914. The head portion 908 may include a tapered surface 924 to facilitate engagement and/or deflection of the fingers 920 via the tabs 922. The shaft 904 is threaded with the threaded bore 916 until the head portion 908 releases, clears or moves past the tabs 922. Once the head portion 908 is adjacent the tabs 922, the fingers 920 spring back toward the shaft 904 or the actuator stem 914 so that the surfaces 924 (e.g., top surfaces) of the tabs 922 engage the shoulder 912 of the shaft 904 to provide a locked condition between the actuator stem 914 and rod end bearing 902. In this manner, the tabs 922 engage the shoulder 912 to provide a locking mechanism or locked condition to prevent the actuator stem 914 from decoupling or disengaging from the rod end bearing 902. As a result, the actuator stem 914 cannot be disassembled from the rod end bearing 902 without manipulation (e.g., from a maintenance person) of the flexible fingers 920.

Thus, when coupled to, for example, the actuator assembly 100 of FIG. 1, the tabs 922 of the fingers 920 engage the shoulder 912 to provide a locking mechanism that prevents the actuator stem 914 from disengaging or decoupling from the rod end bearing 902 when a torque is applied to the fastener 128 (e.g., in a counter-clockwise direction) about an axis 926 when disassembling the diaphragm plate 120 from the actuator stem 912.

The example actuator stems 204, 402, 504, 602, 702, 812, 914 and rod end bearings 210, 404, 508, 604, 706, 802, 902 described herein may be factory installed and/or may be retrofit to existing valves. For example, to retrofit an existing valve such as, for example, the actuator assembly 100 of FIG. 1, the rod end bearing 144 and the actuator stem 122 are removed and replaced with the respective example actuator stems 204, 402, 504, 602, 702, 812, or 914 and rod end bearings 210, 404, 508, 604, 706, 802, or 902. In the examples shown in FIGS. 2, 3A, 3B, 4A-4D, 5, 6A-6C, and 7A-7D, the studs 218, 414, 610, and 704 may be obtained or provided to couple the respective actuator stems 204, 402, 504, 602, 702, 812, or 914 and rod end bearing 210, 404, 508, 604, 706, 802, or 902. The studs 218, 414, 610, and/or 704 may be made of high strength, alloy steel and may be made via machining or any other suitable process(es).

Although certain apparatus have been described herein, the scope of coverage of this patent is not limited thereto. To the contrary, this patent covers all apparatus fairly falling within the scope of the appended claims either literally or under the doctrine of equivalents.

Claims

1. An apparatus for use with a control valve actuator comprising:

a rod end bearing having a bearing retainer and a shaft portion extending from the bearing retainer;
an actuator stem having a first end to be operatively coupled to a diaphragm plate of the control valve actuator and a second end to be coupled to the rod end bearing;
a connector to couple the rod end bearing and the actuator stem, the connector having a non-threaded recessed portion between a first end and a second end of the connector, the first end and the non-threaded recessed portion forming a first shoulder and the second end and the non-threaded recessed portion forming a second shoulder; and
a lock integrally formed with the actuator stem or the rod end bearing, at least a portion of the lock being deformable or deflectable toward the non-threaded recessed portion to engage the first shoulder and the second shoulder when the rod end bearing is coupled to the actuator stem to provide a locked condition, the lock is to restrict or prevent movement of the rod end bearing relative to the actuator stem when the rod end bearing is coupled to the actuator stem to prevent the actuator stem and the rod end bearing from decoupling in a direction along a longitudinal axis of the actuator stem when the actuator stem is coupled or de-coupled to the diaphragm plate.

2. An apparatus of claim 1, wherein the connector comprises a stud.

3. An apparatus of claim 2, wherein the stud includes at least a partially externally threaded body that is received by first and second bores of the actuator stem and rod end bearing to couple the actuator stem to the rod end bearing.

4. An apparatus of claim 1, wherein the lock comprises at least one deformable tab disposed along a body of the actuator stem or the rod end bearing.

5. An apparatus of claim 4, wherein the connector comprises a stud having the non-threaded recessed portion formed between a first threaded portion and a second thread portion, the first end of the connector having the first threaded portion and the second end of the connector having the second threaded portion, the non-threaded recessed portion of the stud and the first threaded portion form the first shoulder and the non-threaded recessed portion and the second threaded portion form the second shoulder.

6. An apparatus of claim 4, wherein the at least one deformable tab engages the first shoulder or the second shoulder when the at least one deformable tab is deformed or deflected toward the non-threaded recessed portion.

7. An apparatus of claim 4, wherein a first tab engages the first shoulder and a second tab engages the second shoulder when the rod end bearing is coupled to the actuator stem and the lock is deformed or deflected.

8. An apparatus of claim 4, wherein the at least one deformable tab is formed on a body of the rod end bearing or on a body of the actuator stem.

9. An apparatus of claim 8, wherein the at least one deformable tab is positioned inward relative to an outer surface of the body of the rod end bearing or an outer surface of the actuator stem when the at least one deformable tab is in the locked condition.

10. An apparatus of claim 1, wherein the first end comprises a first threaded portion and the second end comprises a second threaded portion.

11. An apparatus of claim 1, wherein a diameter of each of the first and second threaded portions is greater than a diameter of the non-threaded recessed portion.

12. An apparatus of claim 1, wherein the rod end bearing includes a first bore to receive the first end of the connector and the actuator stem includes a second bore to receive the second end of the connector.

13. An apparatus of claim 12, wherein each of the first and second bores comprises an internally threaded bore.

14. An apparatus of claim 1, wherein the lock is to prevent axial movement of the rod end bearing relative to the actuator stem in a direction along the longitudinal axis of the actuator stem.

15. An apparatus for use with a control valve actuator comprising:

a rod end bearing having a shaft that includes a threaded opening;
an actuator stem having a threaded opening at a first end of the actuator stem; and
a stud having at least a non-threaded recessed portion positioned between a first threaded portion and a second threaded portion, the first threaded portion of the stud to be received in the threaded opening of the rod end bearing and the second threaded portion of the stud to be received in the threaded opening of the actuator stem to threadably couple the rod end bearing and the actuator stem, at least one of the rod end bearing or the actuator stem including a deformable portion to engage the non-threaded recessed portion to prevent axial movement of the rod end bearing relative to the actuator stem to prevent inadvertent separation of the rod end bearing and actuator stem or to prevent rotation of the rod end bearing relative to the actuator stem in a first direction.

16. An apparatus of claim 15, wherein the deformable portion of the actuator stem or the rod end bearing comprises a tab disposed along a body portion of the actuator stem or the rod end bearing.

17. An apparatus of claim 16, wherein the non-threaded recessed portion forms a first shoulder adjacent the first threaded portion and a second shoulder adjacent the second threaded portion.

18. An apparatus of claim 17, wherein the tab is to engage the first shoulder or the second shoulder when the tab is deformed toward the non-threaded recessed portion.

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Patent History
Patent number: 9062794
Type: Grant
Filed: Jul 8, 2009
Date of Patent: Jun 23, 2015
Patent Publication Number: 20110008098
Assignee: FISHER CONTROLS INTERNATIONAL LLC (Marshalltown, IA)
Inventor: Bryan Quinn Leger (Marshalltown, IA)
Primary Examiner: Victor MacArthur
Application Number: 12/499,389
Classifications
Current U.S. Class: Having Locking Means (403/46)
International Classification: F16C 11/00 (20060101); F16K 31/165 (20060101); F16C 7/02 (20060101); F16B 39/02 (20060101);